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Flight manual LS10-s,-st

 

Issued: December 2011   

TN LS10-02 

4.2

EASA app.

 

4.1

 

Introduction 

Section 4 provides checklists and amplified procedures for the conduct of normal 
operation. Normal procedures associated with optional systems can be found in 
section 9. 
 

4.2

 

  Rigging and derigging, filling the watertanks, refuelling 

4.2.1

 

Rigging 

1.

 

Execute the inspection prior to rigging according to section 4.3 A. 

2.

 

Clean and grease all pins and bushes and all 4 automatic control system 
connectors.  

3.

 

Open the canopy. 

4.

 

Set the airbrake handle to the forward stop and control stick and wingflap 
handle to neutral.  
Always rig inner wings without 15 m or 18 m tips.  
With a helper on the wingtip, push the left wing into place, then the right 
wing.  
Check for correct dihedral. The flaperons should be held at neutral for 
rigging, airbrakes locked. All controls will hook up automatically.  

Caution:

 Make sure that the wing trailing edge is at the same height as its 

counterpart at the fuselage before the controls hook up. Otherwise a ball bearing 
of a control hook up bellcrank (mounted at the wing root) may knock against 
the fuselage-side control and will be damaged. 

Sight through the wing main pin bushings to determine alignment. Push the 
main pins in as far as possible. Turn one handle after the other up to the 
fuselage wall, while pulling out the white securing knob, then release the 
knob back to its locked position. Check the securing. 

5.

 

Insert the wing tip extensions (18 m) into the wing. 
Press in the locking pin with your finger. 
Insert the wing tip until the flaperon connecting pins start to slide into the 
centre-flaperon bushes. 
Strike firmly with the palm of your hand on to the wing tip to lock the wing 
tip extension.  
The rigging of the 15 m wingtips (Option) has to be done in the same 
manner as the wing tip extensions. 

6.

 

Check if you are safe to fly with the fin battery (see Data Placard in cockpit 
or entries in section 6). Insert the battery into place. Connect battery to the 
aircraft electric system and check operation.  

 

Summary of Contents for LS10-s

Page 1: ...the responsible airworthiness authority The new or amended text in the revised page will be indicated by a black vertical line in the right hand margin and the Revision No and the date will be shown...

Page 2: ...issued replaced replaced 0 0 0 October 2009 0 1 see manual amendments 0 2 0 3 0 4 0 5 0 6 0 7 October 2009 1 1 1 October 2009 1 2 1 3 1 4 1 5 1 6 2 App 2 1 October 2009 2 2 2 3 2 4 December 11 2 5 2 6...

Page 3: ...nt Section Page issued replaced replaced 4 App 4 1 October 2009 4 2 December 11 4 3 December 11 4 4 4 5 4 6 4 7 4 8 4 9 4 10 4 11 4 12 4 13 4 14 4 15 4 16 4 17 4 18 4 19 4 20 4 21 4 22 4 23 4 24 4 25...

Page 4: ...ges cont Section Page issued replaced replaced 6 6 1 October 2009 6 2 6 3 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 11 6 12 6 13 December 11 6 14 December 11 7 7 1 October 2009 7 2 December 11 7 3 7 4 7 5 7 6 7...

Page 5: ...LS10 02 0 6 0 2 List of effective pages cont Section page issued replaced replaced 7 25 7 26 7 27 7 28 7 29 7 30 7 31 7 32 7 33 December 11 7 34 December 11 7 35 December 11 7 36 8 8 1 October 2009 8...

Page 6: ...t is maximum speed permissible with flaps extended positive 2 1 Green Arc 97 200 52 108 Normal Operating Range Lower limit is 1 1 VS1 at maximum weight and most forward c g with flaps neutral Upper li...

Page 7: ...keep blinking When reaching the non usable amount of fuel R is displayed and will keep blinking 2 6 Fuel only LS10 st Fuel capacity Fuselage tank total 12 l 3 20 US gal Non usable amount of fuel 0 3...

Page 8: ...g edge is at the same height as its counterpart at the fuselage before the controls hook up Otherwise a ball bearing of a control hook up bellcrank mounted at the wing root may knock against the fusel...

Page 9: ...ions the wing joints and the horizontal stabilizer 12 Execute a positive control check one helper is needed to hold firmly the control surfaces Only LS10 st 13 Pull off the fuel vent surge bottle from...

Page 10: ...1 4 16 13 65 Water in outer wing tank System No 1 up to 30 0 66 1 0 189 0 62 Water in the centre wing tank System No 1 up to 50 0 110 2 0 189 0 62 Water in the inner wing tank System No 2 up to 110 0...

Page 11: ...2 6 kg 5 7 lbs increases Minimum Cockpit Load by 11 2 kg 24 6 lbs Installation of heavy tailwheel mass difference to standard tail wheel 3 kg 6 6 lbs increases Minimum Cockpit Load by 12 9 kg 28 5 lbs...

Page 12: ...r AFRP skin Fuselage CFRP GFRP shell Canopy Large single piece canopy hinged at the front nose and supported by a gas strut Canopy is made of Plexiglas GS clear GS 241 or optionally green GS green 294...

Page 13: ...iometers B Altimeter G Variometer switch Option C Variometer TE Soaring static Engine operstion D Electrical Variometer switch shown in SOARING position Colours of instrument lines 1 Multi Probe Pitot...

Page 14: ...d handle to jettison the canopy 2 As soon as the canopy is lifted by the instrument panel support the person at the front end must hold the canopy so that it will not be lifted more than approx 3 cm 1...

Page 15: ...ent installation of an oxygen system according to its manufacturer instructions by an adequately licensed maintenance repair shop the sailplane including oxygen system must be inspected Weight and Bal...

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